The present invention relates to a military munition of the type having an explosive warhead, and more particularly to a device for separating the warhead from fuze and the adjacent initiator, igniter, detonator, and/or spit-back device (“IIDS device”) that initiates a warhead in a munition. The invention functions to avoid a dangerous condition where such a munition is exposed to external stimuli, such as heat, that could detonate the warhead.
Any munition having an explosive warhead, whether be a grenade, projectile or an assembled munition fitted to a projectile, must function as intended in states and modes of use within the NATO operational conditions:
When munition such as an ammunition cartridge, shell or shoulder launched weapon are stored and when they mention is exposed to heat beyond identified storage conditions (normally in the range of 170° F.) the munitions are subject to premature detonation. For example, the heat generated by a fire increases over time and is generally over a much longer duration (compared to the heat of transferred into a cartridge when it is chambered and dwelling in a cannon barrel). Generally, in slow heating the 1st energetic event is deflagration of the powder. Conversely, in fast heating primers generally initiate ignition.
The present invention provides a mechanism for preventing an unwanted and dangerous detonation of a munition warhead during one of the NATO operational conditions.
When a munition is exposed to unsafe conditions—for example, to heat generated by a fire—the invention harnesses the increasing heat to initiate a dual or triple action vent that physically separates components improving the venting of energetic materials in a manner that precludes a warhead detonation.
A device according to the invention is incorporated into grenades or cartridge munitions and/or into the ammunition's packaging or storage container, a container that may include “dunnage” (dunnage being the internal packaging material in a munitions' container).
A device according to the invention is configured at the physical boundary or interface in a munition where (a) one sub-component includes a warhead containing an explosive and (b) a second sub-component houses the IIDS device that may include a fuse. The invention initiates a two or three step process uncoupling and separating these components at a critical time.
More particularly, the present invention provides a “multi-step separator” for a fuze configured to be mated to an explosive device in a military munition, either at a production facility during manufacture of the munition or during use in the field. The fuze includes a detonator with a booster or spit-back element for initiating an energetic sequence resulting in a high-order detonation of the explosive device. The multi-step separator includes:
One such external stimulus, which activates the separator device, is an elevated temperature, in particular about 160° C., above a range of operational temperatures within which the munition is designed to function. In this case the fuze-munition interface device preferably comprises a solid, fusible material that melts at the elevated temperature, releasing the fuze when it melts.
Alternatively or in addition, the fuze-munition interface device may comprise a shape memory material that changes shape at the elevated temperature, thus releasing the fuze when it changes shape.
According to a preferred embodiment of the invention, the separating device comprises a compressed spring interposed between said fuze and said explosive device. This compressed spring is preferably retained in a compressed state by a first solid, fusible material that melts at an elevated temperature thereby releasing the spring from compression. When and if released, the spring causes the fuze to physically distance itself from the explosive device in the munition.
Alternatively or in addition, the compressed spring is retained in a compressed state by a shape memory material that changes its shape at an elevated temperature thereby releasing the spring from compression.
In a particular, preferred embodiment, the multi-step separator device further comprises a retaining wire configured to allow rotation of the fuze, when and if the fuze is released.
The separator device may also include a housing for the detonator and a second solid, fusible material arranged to release the detonator from the housing when it melts. This second fusible material preferably has a melting temperature that is above the melting temperature of the first fusible material.
Advantageously the separator device further comprises an insulating material configured to guide the heat away from the first fusible material.
When the fuze is mated to an explosive device at a production facility, the munition is preferably packaged in a box that includes a void in the dunnage, allowing for the physical separation of the fuze from the explosive device. If desired the dunnage can be configured to retain an ammunition belt.
For a full understanding of the present invention, reference should now be made to the following detailed description of the preferred embodiments of the invention as illustrated in the accompanying drawings.
The preferred embodiments of the present invention will now be described with reference to
In conditions of a fire, the two-step or three-step function of the invention allows for the eventual “low-order” deflagration of the explosive load and detonation of IIDS devices in conditions where the energetic events are not contained and where the IIDS device is separated from the warhead.
As shown in
As shown in
Multi-Step Separator Elements: The structure and operation of the multi-step separator according to the present invention are illustrated in
Embedded in the fusible ring 16 is a compressed spring 18 (
Packaging or Storage: Ammunition uses UN packaging (see
Separation: When exposed to heat in a specified range (Temperature Range 1) the sub-components are released from each other. This is accomplished by (a) use of either a memory metal that unfastens the loaded warhead from the component housing the IIDS or (b) use of a fusable material that loses its physical strength (see
Segregation: When the heat increases to a higher range (Temperature Range 2) the sub-component pushes the sub-components apart creating adequate segregation (void) between the warhead (see
Rotation or Compromised Spit-back Integrity: When the IDDS includes a spit-back device, it is also necessary to make sure that a spit-back jet does not initiate the warhead. Accordingly, at Temperature Range 3 (a) a rotation is induced by so that the device is not aligned to generate a jet that would impact on the explosive or alternatively, (b) the spit-back device in the ogive is held in place at temperatures below Temperature Range 3. A housing fabricated from a memory metal or fusible material frees the IIDS device from the ogive at temperatures above Temperature Range 3 so that a focused spit-back jet does not hit the warhead (see
In these conditions the device either rotates the sub-component within a packaged container or the IDSS device is released from a housing comprised of a fusible material or memory metal (see
Inclusion of Insulators: The device must function in a normal environment that does include exposure to heat in chambering, and from air friction in ballistic flight. Therefore, the inactivated memory metal or solid fusible material must be encased and fitted within the munition so that heat is attenuated in normal function conditions that may include chambering into a weapon's barrel or in a normal ballistic flight. However, in conditions outside of the barrel where the fuze is attached the warhead, the device shall activate sequentially releasing the fuze and IIDS from the warhead.
There has thus been shown and described a novel military munition which fulfills all the objects and advantages sought therefor. Many changes, modifications, variations and other uses and applications of the subject invention will, however, become apparent to those skilled in the art after considering this specification and the accompanying drawings which disclose the preferred embodiments thereof. All such changes, modifications, variations and other uses and applications which do not depart from the spirit and scope of the invention are deemed to be covered by the invention, which is to be limited only by the claims which follow.
This application claims priority from Provisional Application No. 61/981,298, filed Apr. 18, 2014, entitled “TRIPLE ACTION VENT AND SUB-COMPONENT SEPARATOR.”
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61981298 | Apr 2014 | US |